A study on supersonic mixing flowfield with swept ramp injectors

S. Aso, Y. Yamane, K. Umii, K. Tokunaga, Y. Ando, K. Sakata

Research output: Contribution to conferencePaper

2 Citations (Scopus)

Abstract

In the present study supersonic mixing flows with parallel injectors are investigated experimentally and computationally. In the experiments the flow fields are visualized by the Schlieren method and flow technique. Also surface pressure distributions in the whole region are measured and complicated flow structure is revealed. In the present study three-dimensional full Navier-Stokes equations are solved for simulating three- dimensional supersonic mixing flow problems in detail.The results show the present numerical code could capture the flow structure quantitatively to some extent. Also the results suggest the detailed and reliable experiments can be quite important in set for the code validation of numerical simulations.

Original languageEnglish
Publication statusPublished - Jan 1 1997
Event35th Aerospace Sciences Meeting and Exhibit, 1997 - Reno, United States
Duration: Jan 6 1997Jan 9 1997

Other

Other35th Aerospace Sciences Meeting and Exhibit, 1997
CountryUnited States
CityReno
Period1/6/971/9/97

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All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Aso, S., Yamane, Y., Umii, K., Tokunaga, K., Ando, Y., & Sakata, K. (1997). A study on supersonic mixing flowfield with swept ramp injectors. Paper presented at 35th Aerospace Sciences Meeting and Exhibit, 1997, Reno, United States.